Core, Honeycomb, Glass/Phenolic Bias Weave Fiber Construction
- Aerospace Material Specification
- AMS3716C
- Reaffirmed
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Core, Flexible Honeycomb, Polyamide Paper Base, Phenolic Coated |
| Aerospace Material Specification | Honeycomb Core, Aluminum Alloy, for Sandwich Construction, 5056, 350 (175) |
| Aerospace Material Specification | Cloth, Type "S" Glass 181 Style Fabric, Finish No. HTS-904 |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
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| TABLE 1 | ||
| TABLE 1 | (SI) | |
| TABLE 2A | ||
| TABLE 2B |
Issuing Committee
AMS P17 Polymer Matrix Composites Committee
AMS P-17, Polymer Matrix Composites, is a technical committee in SAE’s Aerospace Materials Systems Group with the responsibility to develop and maintain material specifications and other SAE technical reports for composite materials, including prepregs, reinforcing fibers and fabrics, matrix resins, adhesives, and core materials. The committee works in conjunction with related bodies such as the Composite Materials Handbook -17 (CMH-17), ASTM Committee D30 on Composite Materials, the National Center for Advanced Materials Performance (NCAMP), the Performance Review Institute (PRI), and regulatory authorities such as FAA and EASA.